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Flight Testing of the Space Launch System (SLS) Adaptive Augmenting Control (AAC) Algorithm on an F/A-18The Marshall Space Flight Center (MSFC) Flight Mechanics and Analysis Division developed an adaptive augmenting control (AAC) algorithm for launch vehicles that improves robustness and performance on an as-needed basis by adapting a classical control algorithm to unexpected environments or variations in vehicle dynamics. This was baselined as part of the Space Launch System (SLS) flight control system. The NASA Engineering and Safety Center (NESC) was asked to partner with the SLS Program and the Space Technology Mission Directorate (STMD) Game Changing Development Program (GCDP) to flight test the AAC algorithm on a manned aircraft that can achieve a high level of dynamic similarity to a launch vehicle and raise the technology readiness of the algorithm early in the program. This document reports the outcome of the NESC assessment.
Document ID
20140012788
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Dennehy, Cornelius J.
(NASA Langley Research Center Hampton, VA, United States)
VanZwieten, Tannen S.
(NASA Langley Research Center Hampton, VA, United States)
Hanson, Curtis E.
(NASA Armstrong Flight Research Center Edwards, CA, United States)
Wall, John H.
(Jacobs Technology, Inc. Huntsville, AL, United States)
Miller, Chris J.
(NASA Armstrong Flight Research Center Edwards, CA, United States)
Gilligan, Eric T.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Orr, Jeb S.
(Jacobs Technology, Inc. Huntsville, AL, United States)
Date Acquired
October 2, 2014
Publication Date
September 1, 2014
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
NESC-RP-13-00847
NF1676L-19786
NASA/TM-2014-218528
L-20474
Funding Number(s)
CONTRACT_GRANT: WBS 869021.05.07.09.27
Distribution Limits
Public
Copyright
Public Use Permitted.
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